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GOE 738 AIRFOIL (goe738-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: GOE 738 AIRFOIL (goe738-il)
Reynolds number: 500,000
Max Cl/Cd: 79.33 at α=7.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe738-il-500000-n5.txt
Download as CSV file: xf-goe738-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 738 AIRFOIL                                 
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.000  -0.9962   0.12258   0.11933   0.0002   1.0000   0.0285
 -18.750  -1.0321   0.11139   0.10795  -0.0069   1.0000   0.0287
 -18.500  -1.0607   0.10197   0.09838  -0.0129   1.0000   0.0288
 -18.250  -1.0859   0.09350   0.08976  -0.0182   1.0000   0.0290
 -18.000  -1.1086   0.08569   0.08181  -0.0231   1.0000   0.0292
 -17.750  -1.1287   0.07857   0.07454  -0.0275   1.0000   0.0293
 -17.500  -1.1460   0.07199   0.06782  -0.0316   1.0000   0.0295
 -17.250  -1.1621   0.06591   0.06160  -0.0353   1.0000   0.0296
 -17.000  -1.1743   0.06055   0.05611  -0.0384   1.0000   0.0298
 -16.750  -1.1837   0.05577   0.05118  -0.0412   1.0000   0.0300
 -16.500  -1.1918   0.05142   0.04669  -0.0435   1.0000   0.0302
 -16.250  -1.1971   0.04763   0.04277  -0.0452   1.0000   0.0303
 -16.000  -1.2003   0.04432   0.03933  -0.0465   1.0000   0.0305
 -15.750  -1.2032   0.04127   0.03618  -0.0474   1.0000   0.0307
 -15.500  -1.2060   0.03847   0.03330  -0.0478   1.0000   0.0309
 -15.250  -1.2063   0.03609   0.03086  -0.0478   1.0000   0.0312
 -15.000  -1.2046   0.03407   0.02877  -0.0475   1.0000   0.0314
 -14.750  -1.2021   0.03224   0.02687  -0.0468   1.0000   0.0316
 -14.500  -1.1966   0.03078   0.02535  -0.0459   1.0000   0.0320
 -14.250  -1.1902   0.02946   0.02397  -0.0447   1.0000   0.0323
 -14.000  -1.1832   0.02826   0.02270  -0.0433   1.0000   0.0326
 -13.750  -1.1756   0.02716   0.02153  -0.0417   1.0000   0.0329
 -13.500  -1.1667   0.02618   0.02049  -0.0400   1.0000   0.0332
 -13.250  -1.1411   0.02518   0.01933  -0.0414   0.8991   0.0337
 -13.000  -1.1324   0.02455   0.01847  -0.0389   0.8519   0.0340
 -12.750  -1.1231   0.02392   0.01768  -0.0364   0.8297   0.0343
 -12.500  -1.1125   0.02330   0.01692  -0.0340   0.8140   0.0347
 -12.250  -1.1007   0.02273   0.01622  -0.0317   0.8010   0.0350
 -12.000  -1.0910   0.02205   0.01548  -0.0290   0.7895   0.0354
 -11.750  -1.0779   0.02150   0.01486  -0.0268   0.7800   0.0359
 -11.500  -1.0613   0.02097   0.01426  -0.0251   0.7708   0.0364
 -11.250  -1.0434   0.02047   0.01369  -0.0236   0.7628   0.0369
 -11.000  -1.0244   0.01998   0.01313  -0.0222   0.7548   0.0374
 -10.500  -0.9845   0.01906   0.01205  -0.0197   0.7403   0.0386
 -10.250  -0.9635   0.01862   0.01153  -0.0186   0.7331   0.0392
 -10.000  -0.9419   0.01822   0.01104  -0.0175   0.7267   0.0397
  -9.750  -0.9210   0.01771   0.01050  -0.0164   0.7199   0.0405
  -9.500  -0.8991   0.01729   0.01004  -0.0154   0.7134   0.0413
  -9.250  -0.8762   0.01692   0.00962  -0.0145   0.7074   0.0422
  -9.000  -0.8527   0.01656   0.00922  -0.0137   0.7009   0.0432
  -8.750  -0.8290   0.01624   0.00882  -0.0128   0.6945   0.0443
  -8.500  -0.8050   0.01592   0.00843  -0.0121   0.6888   0.0451
  -8.250  -0.7814   0.01552   0.00802  -0.0113   0.6824   0.0463
  -8.000  -0.7572   0.01520   0.00766  -0.0106   0.6763   0.0476
  -7.750  -0.7325   0.01490   0.00732  -0.0099   0.6708   0.0489
  -7.500  -0.7073   0.01462   0.00700  -0.0093   0.6644   0.0504
  -7.250  -0.6822   0.01435   0.00668  -0.0087   0.6583   0.0519
  -7.000  -0.6572   0.01405   0.00637  -0.0081   0.6530   0.0538
  -6.750  -0.6315   0.01379   0.00610  -0.0075   0.6471   0.0559
  -6.500  -0.6055   0.01358   0.00583  -0.0070   0.6408   0.0579
  -6.250  -0.5801   0.01331   0.00554  -0.0065   0.6350   0.0602
  -6.000  -0.5541   0.01306   0.00529  -0.0060   0.6288   0.0627
  -5.750  -0.5277   0.01287   0.00505  -0.0055   0.6229   0.0651
  -5.500  -0.5018   0.01264   0.00479  -0.0050   0.6174   0.0679
  -5.250  -0.4754   0.01241   0.00457  -0.0046   0.6112   0.0714
  -5.000  -0.4488   0.01223   0.00436  -0.0042   0.6047   0.0747
  -4.750  -0.4227   0.01201   0.00413  -0.0037   0.5989   0.0794
  -4.500  -0.3960   0.01182   0.00394  -0.0033   0.5930   0.0842
  -4.250  -0.3697   0.01160   0.00374  -0.0029   0.5871   0.0913
  -4.000  -0.3434   0.01140   0.00356  -0.0025   0.5815   0.1020
  -3.750  -0.3169   0.01117   0.00341  -0.0021   0.5755   0.1180
  -3.500  -0.2903   0.01099   0.00327  -0.0017   0.5691   0.1339
  -3.250  -0.2635   0.01086   0.00315  -0.0014   0.5634   0.1468
  -3.000  -0.2364   0.01069   0.00303  -0.0011   0.5578   0.1589
  -2.750  -0.2093   0.01056   0.00292  -0.0008   0.5520   0.1695
  -2.250  -0.1549   0.01032   0.00272  -0.0002   0.5411   0.1934
  -2.000  -0.1278   0.01020   0.00263   0.0001   0.5340   0.2073
  -1.750  -0.1010   0.01008   0.00254   0.0005   0.5269   0.2245
  -1.500  -0.0739   0.00994   0.00246   0.0008   0.5198   0.2452
  -1.250  -0.0475   0.00978   0.00238   0.0012   0.5135   0.2734
  -1.000  -0.0212   0.00961   0.00232   0.0016   0.5078   0.3082
  -0.750   0.0048   0.00939   0.00225   0.0020   0.5014   0.3505
  -0.500   0.0301   0.00917   0.00219   0.0026   0.4951   0.4020
  -0.250   0.0552   0.00894   0.00216   0.0032   0.4898   0.4581
   0.000   0.0797   0.00870   0.00214   0.0040   0.4839   0.5226
   0.250   0.1045   0.00854   0.00213   0.0047   0.4773   0.5745
   0.500   0.1304   0.00843   0.00213   0.0053   0.4706   0.6114
   0.750   0.1564   0.00836   0.00214   0.0059   0.4629   0.6438
   1.000   0.1823   0.00832   0.00216   0.0065   0.4569   0.6751
   1.250   0.2087   0.00825   0.00220   0.0070   0.4517   0.7046
   1.500   0.2352   0.00823   0.00224   0.0075   0.4462   0.7332
   1.750   0.2615   0.00821   0.00229   0.0081   0.4409   0.7600
   2.000   0.2885   0.00820   0.00235   0.0085   0.4359   0.7835
   2.250   0.3157   0.00820   0.00240   0.0088   0.4302   0.8051
   2.500   0.3428   0.00819   0.00248   0.0093   0.4245   0.8359
   2.750   0.3730   0.00818   0.00259   0.0091   0.4190   0.8738
   3.000   0.4111   0.00824   0.00273   0.0072   0.4122   0.9062
   3.250   0.4537   0.00840   0.00287   0.0043   0.4050   0.9250
   3.500   0.4922   0.00851   0.00299   0.0023   0.3974   0.9357
   4.000   0.5648   0.00882   0.00323  -0.0011   0.3770   0.9494
   4.250   0.5972   0.00899   0.00336  -0.0020   0.3658   0.9560
   4.500   0.6305   0.00920   0.00350  -0.0031   0.3527   0.9613
   4.750   0.6592   0.00943   0.00366  -0.0034   0.3355   0.9685
   5.000   0.6935   0.00969   0.00384  -0.0048   0.3167   0.9720
   5.250   0.7253   0.00999   0.00405  -0.0058   0.2971   0.9767
   5.500   0.7550   0.01034   0.00430  -0.0064   0.2784   0.9817
   5.750   0.7891   0.01066   0.00453  -0.0080   0.2636   0.9846
   6.000   0.8217   0.01099   0.00479  -0.0093   0.2503   0.9882
   6.250   0.8534   0.01132   0.00506  -0.0103   0.2406   0.9918
   6.500   0.8873   0.01156   0.00529  -0.0118   0.2335   0.9945
   6.750   0.9217   0.01185   0.00555  -0.0135   0.2256   0.9973
   7.000   0.9564   0.01212   0.00580  -0.0152   0.2193   0.9996
   7.250   0.9805   0.01236   0.00604  -0.0147   0.2138   1.0000
   7.500   1.0012   0.01265   0.00632  -0.0135   0.2088   1.0000
   7.750   1.0219   0.01293   0.00659  -0.0124   0.2044   1.0000
   8.000   1.0430   0.01318   0.00686  -0.0113   0.1983   1.0000
   8.250   1.0627   0.01353   0.00718  -0.0100   0.1918   1.0000
   8.500   1.0830   0.01381   0.00748  -0.0088   0.1865   1.0000
   8.750   1.1026   0.01414   0.00780  -0.0076   0.1788   1.0000
   9.000   1.1212   0.01452   0.00815  -0.0062   0.1706   1.0000
   9.250   1.1381   0.01496   0.00856  -0.0047   0.1590   1.0000
   9.500   1.1522   0.01554   0.00905  -0.0028   0.1434   1.0000
   9.750   1.1636   0.01621   0.00964  -0.0005   0.1300   1.0000
  10.000   1.1733   0.01690   0.01029   0.0019   0.1202   1.0000
  10.250   1.1810   0.01760   0.01096   0.0046   0.1128   1.0000
  10.500   1.1817   0.01833   0.01170   0.0083   0.1077   1.0000
  10.750   1.1859   0.01922   0.01260   0.0108   0.1025   1.0000
  11.000   1.1903   0.02036   0.01374   0.0128   0.0973   1.0000
  11.250   1.1992   0.02139   0.01480   0.0141   0.0920   1.0000
  11.500   1.2054   0.02270   0.01611   0.0154   0.0861   1.0000
  11.750   1.2133   0.02398   0.01740   0.0164   0.0806   1.0000
  12.000   1.2196   0.02545   0.01886   0.0173   0.0760   1.0000
  12.250   1.2264   0.02694   0.02037   0.0181   0.0723   1.0000
  12.500   1.2328   0.02851   0.02196   0.0188   0.0698   1.0000
  12.750   1.2391   0.03014   0.02362   0.0194   0.0677   1.0000
  13.000   1.2460   0.03176   0.02528   0.0200   0.0663   1.0000
  13.250   1.2513   0.03354   0.02711   0.0204   0.0647   1.0000
  13.500   1.2561   0.03542   0.02903   0.0208   0.0635   1.0000
  13.750   1.2590   0.03751   0.03116   0.0210   0.0622   1.0000
  14.000   1.2598   0.03986   0.03355   0.0212   0.0607   1.0000
  14.250   1.2647   0.04185   0.03561   0.0214   0.0597   1.0000
  14.500   1.2687   0.04396   0.03778   0.0214   0.0589   1.0000
  14.750   1.2721   0.04623   0.04011   0.0213   0.0576   1.0000
  15.000   1.2747   0.04864   0.04259   0.0212   0.0570   1.0000
  15.250   1.2759   0.05125   0.04526   0.0209   0.0561   1.0000
  15.500   1.2767   0.05398   0.04804   0.0205   0.0554   1.0000
  15.750   1.2772   0.05677   0.05089   0.0201   0.0549   1.0000
  16.000   1.2735   0.06010   0.05426   0.0195   0.0537   1.0000
  16.250   1.2731   0.06310   0.05733   0.0189   0.0530   1.0000
  16.500   1.2759   0.06574   0.06005   0.0183   0.0525   1.0000
  16.750   1.2767   0.06866   0.06305   0.0177   0.0520   1.0000
  17.000   1.2776   0.07157   0.06604   0.0170   0.0514   1.0000
  17.250   1.2783   0.07458   0.06912   0.0163   0.0508   1.0000
  17.500   1.2776   0.07779   0.07241   0.0154   0.0503   1.0000
  17.750   1.2769   0.08102   0.07570   0.0145   0.0494   1.0000
  18.000   1.2740   0.08459   0.07933   0.0134   0.0486   1.0000
  18.250   1.2708   0.08826   0.08305   0.0123   0.0478   1.0000
  18.500   1.2671   0.09201   0.08686   0.0110   0.0472   1.0000
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